Stability. Effect on stability and control of pusher propeller behind conventional tail surfaces as determined by tests of powered model in free-flight tunnel [with one reference]; by John P. Campbell and Thomas A. Hollingworth.
Publication Title:
Stability. Effect on stability and control of pusher propeller behind conventional tail surfaces as determined by tests of powered model in free-flight tunnel [with one reference]; by John P. Campbell and Thomas A. Hollingworth.
Display Title:
Stability. Effect on stability and control of pusher propeller behind conventional tail surfaces as determined by tests of powered model in free-flight tunnel [with one reference]; by John P. Campbell and Thomas A. Hollingworth.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Campbell, John P. and Hollingworth, Thomas A.
Date:
[1946.]
Publish Date ISO Format:
1946-01-01T00:00:00Z
Publication Start:
19460101
Publication End:
19461231
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
13
Publication year:
1946
SuDoc number:
Y 3.N 21/5:11/L-220
Description:
cover title, 20 p. 16 pl. 4°
Notes:
(Wartime report L-220.) [Processed. Originally issued Jan. 1943 as Advance confidential report.]
Notes:
(Wartime report L-220.) [Processed. Originally issued Jan. 1943 as Advance confidential report.] † Distribution Made by Issuing Office.